Low-altitude aircraft transparent part
By using the process of integral molding of the base body, UR layer and composite diaphragm layer in the mold in the production of transparent parts of low-altitude aircraft, the problems of complex production processes, time-consuming and high cost in the prior art are solved, and efficient production and performance improvement of the product are achieved.
Patent Information
- Application Number
- CN202421387106.7
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-06-18
- Publication Date
- 2025-03-18
- Estimated Expiration
- 2034-06-18
AI Technical Summary
The production process of existing low-altitude aircraft transparent parts is complex, time-consuming, low efficiency, and high cost, making it difficult to meet the requirements of scratch resistance and weather resistance.
The process of integral molding of the substrate body, the UR layer and the composite diaphragm layer in the mold is adopted. The composite diaphragm layer is formed on the inner side of the substrate body and the PUR layer is formed on the outer surface. The performance of the transparent parts is improved through in-film reaction molding and hardening coating.
It greatly reduces production costs and time, improves the production efficiency and qualification rate of the product, improves the toughness, heat resistance, scratch resistance and weather resistance of transparent parts, and can meet the requirements of bird collision experiments.